forked from Archive/PX4-Autopilot
land_detector add missing header and init all vtol fields (#7754)
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@ -46,14 +46,7 @@
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namespace land_detector
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{
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VtolLandDetector::VtolLandDetector() :
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_paramHandle(),
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_params(),
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_airspeedSub(-1),
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_vehicle_status_sub(-1),
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_airspeed{},
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_was_in_air(false),
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_airspeed_filtered(0)
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VtolLandDetector::VtolLandDetector()
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{
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_paramHandle.maxAirSpeed = param_find("LNDFW_AIRSPD_MAX");
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}
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@ -76,7 +69,6 @@ void VtolLandDetector::_update_topics()
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bool VtolLandDetector::_get_maybe_landed_state()
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{
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// Only trigger in RW mode
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if (!_vehicle_status.is_rotary_wing) {
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return false;
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@ -42,6 +42,7 @@
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#pragma once
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#include <uORB/topics/airspeed.h>
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#include <uORB/topics/vehicle_status.h>
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#include "MulticopterLandDetector.h"
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@ -60,24 +61,23 @@ protected:
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bool _get_landed_state() override;
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bool _get_maybe_landed_state() override;
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private:
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struct {
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param_t maxAirSpeed;
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} _paramHandle;
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} _paramHandle{};
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struct {
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float maxAirSpeed;
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} _params;
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} _params{};
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int _airspeedSub;
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int _vehicle_status_sub;
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int _airspeedSub{-1};
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int _vehicle_status_sub{-1};
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struct airspeed_s _airspeed;
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struct vehicle_status_s _vehicle_status;
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airspeed_s _airspeed{};
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vehicle_status_s _vehicle_status{};
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bool _was_in_air; /**< indicates whether the vehicle was in the air in the previous iteration */
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float _airspeed_filtered; /**< low pass filtered airspeed */
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bool _was_in_air{false}; /**< indicates whether the vehicle was in the air in the previous iteration */
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float _airspeed_filtered{0.0f}; /**< low pass filtered airspeed */
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};
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